EP2530246A3 - Système de montage de pièce de transition de chambre de combustion pour cadre de moteur de turbine à gaz - Google Patents
Système de montage de pièce de transition de chambre de combustion pour cadre de moteur de turbine à gaz Download PDFInfo
- Publication number
- EP2530246A3 EP2530246A3 EP12169885.6A EP12169885A EP2530246A3 EP 2530246 A3 EP2530246 A3 EP 2530246A3 EP 12169885 A EP12169885 A EP 12169885A EP 2530246 A3 EP2530246 A3 EP 2530246A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- transition piece
- combustor transition
- frame
- mounting
- gas turbine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 230000007704 transition Effects 0.000 title abstract 4
- 238000011144 upstream manufacturing Methods 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/40—Movement of components
- F05D2250/41—Movement of components with one degree of freedom
- F05D2250/411—Movement of components with one degree of freedom in rotation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/152,117 US8997501B2 (en) | 2011-06-02 | 2011-06-02 | System for mounting combustor transition piece to frame of gas turbine engine |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2530246A2 EP2530246A2 (fr) | 2012-12-05 |
EP2530246A3 true EP2530246A3 (fr) | 2014-04-16 |
EP2530246B1 EP2530246B1 (fr) | 2019-10-23 |
Family
ID=46148760
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP12169885.6A Active EP2530246B1 (fr) | 2011-06-02 | 2012-05-29 | Système de montage de pièce de transition de chambre de combustion pour cadre de moteur de turbine à gaz |
Country Status (3)
Country | Link |
---|---|
US (1) | US8997501B2 (fr) |
EP (1) | EP2530246B1 (fr) |
CN (1) | CN102808697B (fr) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9322335B2 (en) * | 2013-03-15 | 2016-04-26 | Siemens Energy, Inc. | Gas turbine combustor exit piece with hinged connections |
US9321115B2 (en) * | 2014-02-05 | 2016-04-26 | Alstom Technologies Ltd | Method of repairing a transition duct side seal |
US20160047313A1 (en) * | 2014-08-15 | 2016-02-18 | General Electric Company | Bushing for joining turbomachine components |
WO2016093829A1 (fr) * | 2014-12-11 | 2016-06-16 | Siemens Aktiengesellschaft | Support de conduit de transition et procédé pour produire un niveau réglé de rigidité de support |
EP3088691B1 (fr) | 2015-04-27 | 2019-06-19 | Ansaldo Energia Switzerland AG | Procédé de démontage d'une turbine à gaz |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6662567B1 (en) * | 2002-08-14 | 2003-12-16 | Power Systems Mfg, Llc | Transition duct mounting system |
US20090145137A1 (en) * | 2007-12-10 | 2009-06-11 | Alstom Technologies, Ltd., Llc | Transition duct assembly |
US20090188258A1 (en) * | 2008-01-29 | 2009-07-30 | Alstom Technologies Ltd. Llc | Altering a natural frequency of a gas turbine transition duct |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4422288A (en) * | 1981-03-02 | 1983-12-27 | General Electric Company | Aft mounting system for combustion transition duct members |
CN2086813U (zh) * | 1990-11-30 | 1991-10-16 | 姜琴弟 | 摇头电扇摆角无级调节装置 |
US5414999A (en) | 1993-11-05 | 1995-05-16 | General Electric Company | Integral aft frame mount for a gas turbine combustor transition piece |
JPH10196402A (ja) * | 1997-01-08 | 1998-07-28 | Toshiba Corp | ガスタービン燃焼器吊り装置およびその運用方法 |
US6216442B1 (en) * | 1999-10-05 | 2001-04-17 | General Electric Co. | Supports for connecting a flow sleeve and a liner in a gas turbine combustor |
US6442946B1 (en) * | 2000-11-14 | 2002-09-03 | Power Systems Mfg., Llc | Three degrees of freedom aft mounting system for gas turbine transition duct |
JP2002243154A (ja) * | 2001-02-16 | 2002-08-28 | Mitsubishi Heavy Ind Ltd | ガスタービン燃焼器尾筒出口構造及びガスタービン燃焼器 |
US7137241B2 (en) * | 2004-04-30 | 2006-11-21 | Power Systems Mfg, Llc | Transition duct apparatus having reduced pressure loss |
US7082766B1 (en) * | 2005-03-02 | 2006-08-01 | General Electric Company | One-piece can combustor |
US7377117B2 (en) * | 2005-08-09 | 2008-05-27 | Turbine Services, Ltd. | Transition piece for gas turbine |
JP5010521B2 (ja) * | 2008-03-28 | 2012-08-29 | 三菱重工業株式会社 | 燃焼器尾筒案内治具及びガスタービンの燃焼器の取り外し方法、並びに製造方法 |
US20090249791A1 (en) * | 2008-04-08 | 2009-10-08 | General Electric Company | Transition piece impingement sleeve and method of assembly |
US8051662B2 (en) * | 2009-02-10 | 2011-11-08 | United Technologies Corp. | Transition duct assemblies and gas turbine engine systems involving such assemblies |
-
2011
- 2011-06-02 US US13/152,117 patent/US8997501B2/en active Active
-
2012
- 2012-05-29 EP EP12169885.6A patent/EP2530246B1/fr active Active
- 2012-06-01 CN CN201210178178.6A patent/CN102808697B/zh not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6662567B1 (en) * | 2002-08-14 | 2003-12-16 | Power Systems Mfg, Llc | Transition duct mounting system |
US20090145137A1 (en) * | 2007-12-10 | 2009-06-11 | Alstom Technologies, Ltd., Llc | Transition duct assembly |
US20090188258A1 (en) * | 2008-01-29 | 2009-07-30 | Alstom Technologies Ltd. Llc | Altering a natural frequency of a gas turbine transition duct |
Also Published As
Publication number | Publication date |
---|---|
CN102808697A (zh) | 2012-12-05 |
US8997501B2 (en) | 2015-04-07 |
EP2530246B1 (fr) | 2019-10-23 |
CN102808697B (zh) | 2016-10-19 |
EP2530246A2 (fr) | 2012-12-05 |
US20120304664A1 (en) | 2012-12-06 |
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